Interesting site!
DM 5.12
http://www.khai.edu/niipfm/english/dm512-en.htm
This was used to test early configurations for the Mikoyan 1.42 in 1986-1992.
The models had the modular design concept. The versions of aerodynamic layout permitting to realize controlled high-angle-of-attack flight under the full airflow breakaway were completed with these models. The problems of aerodynamic and gas-dynamic control methods combination, control system structure and laws were investigated during the flight tests at supercritical angles of attack, under the stall and spin conditions.
The obtained research results allowed to receive a series of advanced aerodynamic layouts for high manoeuvering aircraft.
These models were used in the Berkut program
http://www.khai.edu/niipfm/english/slm22-en.htm
SLM-22
The following research programs were performed with the model:
Research of stability, controllability, stall, spin and methods of spin recovery for an aircraft with the forward-swept wing and different control laws also;
Research of pressure distribution, air vortexes trajectories and airflow over the surfaces of plane units visualization;
Research of air consumption through the engine gas flow duct effect to the stability and controllability characteristics.
http://www.khai.edu/niipfm/english/slm32-en.htm
The model was created in period from 1988 to 1992 and tested till 1999.
The model was the further development of SLM-22 model. It was equipped with turbojet engine.
The following research programs were performed with the model:
Research of stability, controllability, stall, spin and methods of spin recovery for an aircraft with the forward-swept wing and different control laws also;
Research of effect of power plant operation mode to the streamlining, stability, controllability, stall and spin characteristics.
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